• 제목/요약/키워드: Robust Observer

검색결과 442건 처리시간 0.021초

공압 매니퓰레이터의 강인 힘제어 (Robust Force Control of Pneumatic Manipulator)

  • 박정규;노리츠구토시로
    • 대한기계학회논문집A
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    • 제20권2호
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    • pp.540-552
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    • 1996
  • In this paper, a compensation method of disturbance using a disturbance observer is proposed for a force control of a pneumatic robot manipulator. The generated torque by a pneumatic actuator can be estimated based on the pressure signals. The inner torque control system is constructed by feeding back the generated torque to improve the dynamic characteristics of the actuator. In order to reduce the influence of disturbances comprising friction torque, parameter variations of plant and environment and so on, the reaction torque control system is constructed with a disturbance observer which estimates the disturbances based on the reference input to the inner torque control system and the reaction torque sensed with a forced sensor. From some simulations and experiments, it is confirmed that the proposed control system is effective to improve the robustness for the friction torque and the parameter change of object in the force control of a pneumatic robot manupulator.

RBF 신경회로망을 이용한 교류 동기 모터의 강인 속도 제어 (Robust Speed Control of AC Permanent Magnet Synchronous Motor using RBF Neural Network)

  • 김은태;이성열
    • 전자공학회논문지SC
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    • 제40권4호
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    • pp.243-250
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    • 2003
  • 본 논문에서는 RBF 신경망 외란 관측기를 이용한 영구자석형 동기모터의 속도추종 제어기를 제안한다. 먼저 공칭 모델에 대하여 입출력 선형화에 기반한 속도 제어기를 설계하고 RBF 신경망 외란 관측기에 의해 시스템의 블확실성을 보상한다. 시스템의 파라미터와 부하 토크의 변동을 동시에 추정하는 RBF 신경망 외란 관측기를 이용함으로써 제안한 제어 알고리즘은 시스템의 불화실성에 강인한 특성을 갖는다. 마지막으로 모의실험을 통하여 제안된 제어기의 타당성을 검증한다.

필드로봇의 궤적 추종에 대한 강인제어 (Robust Control for Trajectory Tracking Control of Field Robot)

  • 최종환;김승수;양순용;이병룡;안경관;이진걸
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2002년도 추계학술대회 논문집
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    • pp.463-466
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    • 2002
  • The Field Robot means the machinery applied for outdoor tasks in construction, agriculture and undersea etc. In this paper, to field-robotize a hydraulic excavator, we have proposed a robust and systematic controller design method. Disturbance observer is used as inner controller to reshape the excavating system into the linear dynamics of nominal model by compensating coupled nonlinear terms, model uncertainties and external load variations. Using the linear model that is obtained through off-line system identification, a H control scheme is applied to construct a disturbance observer and a servo-controller systematically.

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외란관측기를 갖는 SMC에 의한 DC모터의 강인한 속도제어 (Robust speed control for DC motor based on sliding mode with a disturbance observer)

  • 정태영
    • 수산해양기술연구
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    • 제55권4호
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    • pp.402-410
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    • 2019
  • This paper deals with the disturbance observer (DOB) based sliding mode control (SMC) for a DC motor to control motor rotating speed precisely and to ensure strong robustness against disturbance including load torque and parameter variation. The reason of steady state error in speed on conventional SMC without DOB is analyzed in detail. Especially, the suggested DOB is designed to prevent measuring noise and harmonics caused by derivative operation on rotating speed. The control performance of the DOB based SMC is evaluated by the various simulations. The simulation results showed that the DOB based SMC had more robust performance than the SMC system without DOB. Especially, precise speed control was possible even though motor parameter variation and load torque was added to the system.

고이득 외란 관측기에 기반한 입력 제약 조건이 있는 불확실한 선형 시스템의 강인 추종 제어 (Robust Tracking of Constrained Uncertain Linear Systems using a High-gain Disturbance Observer)

  • 윤문채;김정수;백주훈
    • 제어로봇시스템학회논문지
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    • 제22권6호
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    • pp.397-402
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    • 2016
  • This paper proposes a robust tracking control for constrained uncertain linear systems by combining a disturbance observer (DOB) and linear matrix inequality (LMI) based state feedback control. To this end, the state feedback control is designed for the nominal system and then a DOB based feed-forward control is added to reject uncertainties. In doing so, the DOB and state feedback controller are joined in a way that the combined control satisfies the input constraints and closed loop stability is guaranteed. Simulation results are provided to show that the proposed control scheme successfully stabilizes uncertain systems.

CMAC 신경망 외란관측기를 이용한 유연관절 로봇의 강인 추적제어 (Robust Tracking Control of a Flexible Joint Robot System using a CMAC Neural Network Disturbance Observer)

  • 김은태
    • 전자공학회논문지SC
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    • 제40권5호
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    • pp.299-307
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    • 2003
  • CMAC 신경망은 지역적 구조로 비선형제어에 적용 시 좋은 성능을 보이는 것이 잘 알려져 있다. 본 논문에서는 CMAC 신경망 외란관측기와 제어기를 제안하고 이를 유연관절 로봇의 강인 추적제어에 적용하도록 한다. 이때 CMAC 신경망 외란관측기는 기계시스템에서 발생하는 파라미터의 불확실성과 외부 외란을 상쇄하는 역할을 한다. 컴퓨터 모의 실험을 통하여 본 논문에서 제안한 CMAC 외란관측기를 유연관절 로봇의 제어에 적용하고 그 성능을 확인하도록 한다.

Design of a Robust Stable Flux Observer for Induction Motors

  • Huh, Sung-Hoi;Seo, Sam-Jun;Choy, Ick;Park, Gwi-Tae
    • Journal of Electrical Engineering and Technology
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    • 제2권2호
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    • pp.280-285
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    • 2007
  • This paper presents a robustly adaptive flux observer for speed-sensorless induction motor control. The proposed approach employs additional robustifying signals to cope with the parametric uncertainties instead of designing an estimator, which has been normally used in power electronic drives. For that, the sliding-mode like adaptive controls are designed and their gain parameters are determined so that the observer dynamics are stable in the sense of Lyapunov, and furthermore they can guarantee the robustness against parametric uncertainties in induction motor systems. Estimated rotor speed is to be used to generate feedback control signal for the speed sensorless vector control system. To show the validity and efficiency of the proposed system, simulation results are presented.

출력관측 오차의 필터링을 이용한 비선형 계통의 강인한 신경망 관측기 설계 (Robust Adaptive Neural-Net Observer for Nonlinear Systems Using Filtering of Output Estimation Error)

  • 박장현;윤필상;박귀태
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2001년도 하계학술대회 논문집 D
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    • pp.2320-2322
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    • 2001
  • This paper describes the design of a robust adaptive neural-net(NN) observer for uncertain nonlinear dynamical system. The Lyapunov synthesis approach is used to guarantee a uniform ultimate boundedness property of the state estimation error, as well as of all other signals in the closed-loop system. Especially, for reducing the dynamic oder of the observer, we propose a new method in which no strictly positive real(SPR) condition is needed with on-line estimation of weights of the NNs. No a priori knowledge of an upper bounds on the uncertain terms is required. The theoretical results are illustrated through a simulation example.

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성능지표 선정을 통한 강인한 칼만필터 설계 (Robust Kalman Filter Design via Selecting Performance Indices)

  • 정종철;허건수
    • 대한기계학회논문집A
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    • 제29권1호
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    • pp.59-66
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    • 2005
  • In this paper, a robust stationary Kalman filter is designed by minimizing selected performance indices so that it is less sensitive to uncertainties. The uncertainties include not only stochastic factors such as process noise and measurement noise, but also deterministic factors such as unknown initial estimation error, modeling error and sensing bias. To reduce the effect on the uncertainties, three performance indices that should be minimized are selected based on the quantitative error analysis to both the deterministic and the stochastic uncertainties. The selected indices are the size of the observer gain, the condition number of the observer matrix, and the estimation error variance. The observer gain is obtained by optimally solving the multi-objectives optimization problem that minimizes the indices. The robustness of the proposed filter is demonstrated through the comparison with the standard Kalman filter.

강인한 관측기와 제어기를 적용한 공탄성 시스템의 응답특성 연구 (A Study on the Response Characteristics of Aeroelastic Systems Applying Robust Observer and Controller)

  • 정인주;나성수
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 추계학술대회논문집
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    • pp.115-120
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    • 2004
  • This paper concerns the active aeroelastic control of flapped wing systems exposed to blast and/or the sonic boom in an incompressible flow field. This is achieved via implementation of a robust estimation capability (sliding mode observer: SMO), and of the use of the deflected flap as to suppress the flutter instability or enhance the subcritical aeroelastic response to blast loads. To this end, a control methodology using LQG(Linear Quadratic Gaussian) in conjunction with SMO is implemented, and its performance toward suppressing flutter and reducing the vibrational level in the subcritical flight speed range is demonstrated. Moreover, its performances are compared to the ones provided via implementation of conventional LQG with Kalman filter.

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